N309UP

Service difficulty reports · 172

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N309UP' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA09656496Floorbeam · crackedINSPECTION TYPE:7C MAIN DECK BS 246 LBL 27 FLOORBEAM WEB FOUND CRACK. MAIN DECK BS 246 LBL 27 FLOORBEAM WEB REPAIRED AS PER HX RS NO. R53-15-36357 REV A. THIS REPAIR IS CLASSIFIED AS TIME LIMITED UNTIL JUN 25, 2010. PENDING COMPLETION OF THE FATIGUE AND DAMJun 23, 2009 · N309UP · Boeing 76734AF · Fuselage Main, Floor BeamSDR IPXA09656480Skin · misrepairedINSPECTION TYPE:7C SURVEY SEQUENCE 309-W3-06 LT WING NR 4 SLAT OSS 647 NOSE SKIN REPAIR FASTENER SPACING IS DIFFERENT AS PER SRM. SURVEY SEQUENCE 309-W3-06 LT WING NR 4 SLAT NOSE SKIN AT OSS647 REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44, THIS REPAIR IS CJun 22, 2009 · N309UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09656429Fairing · delaminatedINSPECTION TYPE:C LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5A (1) FIG 5 REV 44.Jun 19, 2009 · N309UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09656428Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B L/E FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5A (1) FIG 5 REV 44.Jun 19, 2009 · N309UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09656498Skin · misrepairedINSPECTION TYPE:7C SURVEY SEQUENCE 309-F1-01 FUSELAGE BETWEEN BS 385 TO 400 AND STR 30R - 32R EXISTING REPAIR PATCH DOES NOT CORRELATE TO A SRM. FUS SKIN REPAIRED AS PER RS NO. R53-10-36353 REV A & IPXA EO NO. B767-5330-33985-A. THIS REPAIR IS CLASSIFIED AS Jun 18, 2009 · N309UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA09656495Rib · crackedINSPECTION TYPE:7C RT WING I/B AILERON I/B HINGE SUPPORT RIB UPPER AFT FLANGE FOUND CRACKED. RT WING I/B AILERON I/B HINGE SUPPORT FIG RIB REPAIR AS PER HX RS NO. 57-55-36355 REV A. THIS IS A PERMANENT REPAIR WITH MATERIAL AND 10133-2002-7075T6511 AS REPAIR Jun 18, 2009 · N309UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA09656481Skin · crackedINSPECTION TYPE:7C LT WING NR 4 SLAT NOSE SKIN I/B SUPPORT WEB FASTENER HOLE AREA FOUND CRACKED. LT WING NR 4 SLAT NOSE SKIN AT OSS572-875 REPAIR AS PER SRM 57-43-01-2R2, FIG 201, REV 44. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATERIAL 7075-0-0071IJun 18, 2009 · N309UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09656435Slat · chafedINSPECTION TYPE:C LT WING NR 1 SLAT LOWER AREA AT O/B AUX TRACK FOUND CHAFE. METAL HOT BOND REPAIR PERFORMED AS PER SRM REV 44, 51-70-10 REPAIR 4 FIG 202.Jun 18, 2009 · N309UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09656432Skin · crackedINSPECTION TYPE:C RT WING NR 9 SLAT NOSE SKIN I/B SUPPORT WEB FASTENER HOLE AREA FOUND CRACKED (0.125 INCH LENGTH). RT WING NR 9 SLAT NOSE SKIN AT OSS 572.875 REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MJun 18, 2009 · N309UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09656431Skin · crackedINSPECTION TYPE:C RT WING NR 9 SLAT NOSE SKIN O/B SUPPORT WEB FASTENER HOLE AREA FOUND CRACKED (0.125 INCH LENGTH). RT WING NR 9 SLAT NOSE SKIN AT OSS 641.615 REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MJun 18, 2009 · N309UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA09656430Skin Panel · delaminatedINSPECTION TYPE:C EMP - VERTICAL STAB LT EXTERIOR SURFACE FWD MIDDLE AREA FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REV 44, REPAIR 4 FIG 201.Jun 18, 2009 · N309UP · Boeing 76734AF · Vertical Stabilizer, Plate/SkinSDR IPXA09656409Floor Panel · crackedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND CRACK 2 INCH LONG AT STA 975 TO STA 1043 LBL 33 TO LBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jun 18, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656399Floor Panel · puncturedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND PUNCTURED AT STA 650 RBL 6. FLOOR PANEL REPAIR AS PER SRM 53-00-50-2R FIG 201, REV 44.Jun 18, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656398Floor Panel · puncturedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND PUNCTURED AT STA 1452 RBL 48. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R FIG 201 REV 44.Jun 18, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656397Floor Panel · puncturedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND PUNCTURED AT STA 1580 LBL 28. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R FIG 201 REV 44.Jun 18, 2009 · N309UP · Boeing 767* · Fuselage Floor PanelSDR IPXA09656497Skin · dentedINSPECTION TYPE:7C SURVEY SEQUENCE 309-F1-02 FX BS 443 TO BS 460 & STR 22R - 25R EXISTING REPAIR DOUBLER CLOSE TO FWD CARGO DOOR CUTOUT. DENT REVEALED AND NO CUTOUT FOUND. SURVEY SEQUENCE 309-F1-02 FUSELAGE BETWEEN BS 443 TO BS 460 AND STR 22R - 25R SKIN REPJun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA09656476Attach Fitting · crackedINSPECTION TYPE:7C MAIN E/E COMPT STA 246 RBL 10 MAIN DECK FLOOR SUPPORT BEAM ATT CLIP AT FRONT SURFACE FOUND CRACK. MAIN E/E COMPT STA 246 RBL 10 MAIN DECK FLOOR SUPPORT BEAM ATT CLIP AT FRONT SURFACE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Main, Attach FittingsSDR IPXA09656474Attach Fitting · crackedINSPECTION TYPE:7C RT WING - L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP FOUND CRACKED. RT WING - L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.Jun 17, 2009 · N309UP · Boeing 76734AF · Wing, Attach FittingsSDR IPXA09656473Attach Fitting · crackedINSPECTION TYPE:7C RT WING L/E LES 546 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP FOUND CRACKED. RT WING L/E LES 546 FIXED FAIRING UPPER SUPPORT WEB AFT FRONT SPAR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.Jun 17, 2009 · N309UP · Boeing 76734AF · Wing, Attach FittingsSDR IPXA09656437Attach Fitting · crackedINSPECTION TYPE:C MAIN E/E COMPT STA 246 LBL 50 MAIN DECK FLOOR SUPPORT BEAM ATT CLIP AT REAR SURFACE FOUND CRACKED (0.75 INCH LENGTH). MAIN E/E COMPT STA 246 LBL 50 MAIN DECK FLOOR SUPPORT BEAM ATT CLIP AT REAR SURFACE REPLACED AS PER SRM 51-10-02 AND INSTALJun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09656436Attach Angle · crackedINSPECTION TYPE:C MAIN E/E COMPT STA 246 LBL 25 MAIN DECK FLOOR SUPPORT BEAM ATT ANGLE AT FRONT SURFACE FOUND CRACK (CRACK 0.5 INCH LENGTH. MAIN E/E COMPT STA 246 LBL 25 MAIN DECK FLOOR SUPPORT BEAM ATT ANGLE REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09656427Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1480 TO STA 1598 LBL 11 TO RBL 11. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656426Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1197+22 TO STA 1207 LBL 11 TO RBL 11. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656425Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1207 TO STA 1344 LBL 11 TO RBL 11. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656424Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 654+22 TO STA 690 LBL 11 TO RBL 11. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656423Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1344 TO STA 1480, LBL 77 TO LBL 88. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656422Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGE AT STA 1430 TO STA 1540, LBL 55 TO LBL 77. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656421Floor Panel · damagedINSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 412 TO STA 550, LBL 77 TO LBL 88. FLOOR PNL FABRICATED AS PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656414Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 412 TO STA 540, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656413Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 412 TO STA 540, LBL 55 TO LBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656412Floor Panel · damagedINSPECTION TYPE:N/A MCD FLOOR PANEL FOUND DAMAGE AT STA 540 TO STA 654+22 LBL 33 TO LBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-11-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656411Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 412 TO STA 540, RBL 55 TO RBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656410Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 731 TO STA 833, RBL 33 TO RBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656408Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 1197+132 TO STA 1207 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656407Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 1197+22 TO STA 1207, RBL 55 TO RBL 77. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656406Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 550 TO STA 654+22 LBL 77 TO LBL 88. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656405Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 654+22 TO STA 690, LBL 33 TO LBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656403Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 731 TO STA 833, LBL 33 TO LBL 55. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656402Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 930 TO STA 975, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693F AND INSTALLED AS PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656401Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 833 TO STA 930 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656400Floor Panel · damagedINSPECTION TYPE:7C MCD FLOOR PANEL FOUND DAMAGE AT STA 975 TO STA 1114 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED AS PER EO B767-5320-9693-F AND INSTALLED AS PER AMM 53-01-01.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09656377Fitting · crackedINSPECTION TYPE:6C AFT CARGO STA 1087 LBL 25 BELOW FLOOR SUPPORT CLIP FOUND CRACK. AFT CARGO COMPT BS 1087 LBL 25 BELOW FLOOR SUPPORT ATT ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09656376Fitting · crackedINSPECTION TYPE:6C AFT CARGO STA 1087 RBL 25 BELOW FLOOR SUPPORT CLIP FOUND CRACK. AFT CARGO COMPT BS 1087 RBL 25 BELOW FLOOR SUPPORT ATT ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.Jun 17, 2009 · N309UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR IPXA09656475Attach Fitting · crackedINSPECTION TYPE:7C LT WING L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AT FRONT SPAR CLIP FOUND CRACKED. LT WING L/E LES 675 FIXED FAIRING UPPER SUPPORT WEB AT FRONT SPAR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.Jun 16, 2009 · N309UP · Boeing 76734AF · Wing, Attach FittingsSDR IPXA09656439Stiffener · crackedINSPECTION TYPE:C CENTER WING TANK FRONT SPAR VERTICAL STIFFENER CRACKED AT BS 786 RBL 10, JUST BELOW CABIN FLOOR (CRACK 3.25 INCH LENGTH). CTR WING TANK FRONT SPAR VERT STIFFENER AT BS 786 RBL 10 AREA REPAIRED AS PER HX RS R57-10-36354 REV A & UPS EO B767-57Jun 16, 2009 · N309UP · Boeing 76734AF · Wing, Center BoxSDR IPXA09656438Hinge Fitting · crackedINSPECTION TYPE:C RT WING I/B MAIN FLAP I/B AFT FLAP HINGE ARM FTG FOUND CRACKED (CRACK 1.5 INCH LENGTH). RT WING I/B MAIN FLAP I/B AFT FLAP HINGE ARM FTG REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATERJun 16, 2009 · N309UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA09656404Hinge Fitting · crackedINSPECTION TYPE:C LT WING I/B MAIN FLAP I/B AFT FLAP HINGE ARM FTG FOUND CRACKED (CRACK 1.5 INCH LENGTH). LT WING I/B MAIN FLAP I/B AFT FLAP HINGE ARM FTG REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATERJun 16, 2009 · N309UP · Boeing 76734AF · Wing, Control Surface Attach FittingsSDR IPXA09656255Latch · bindingCOCKPIT LIFE RAFT STOWAGE COMPT LATCH BINDING, RESTRICTING ACCESS. CHECKED, ADJUSTED AND LUBRICATED LATCH. OPS CHECK GOOD. OK FOR SERVICE.Jun 7, 2009 · N309UP · Boeing 767300 · Life RaftSDR IPXA09655816Floor Panel · dentedINSPECTION TYPE:N/A POS 8L SIDE AT FWD END 3RD PNL FROM LT SIDE DENTED. REPAIRED PER SRM 53-00-50-2R.May 10, 2009 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA09655145Engine · bird ingestionINSPECTION TYPE: ETOP ATB - AFTER DEPARTURE THE CAPTAIN REPORTED TO FLIGHT CONTROL VIA ACARS A BIRD STRIKE WITH POSSIBLE ENGINE AND/OR AIRFRAME DAMAGE. VIBRATION WAS REPORTED ON THE RIGHT ENGINE. REMOVED AND REPLACED RT ENGINE PER TC 6002. ENG TEST C/W PERMar 24, 2009 · N309UP · Boeing 76734AF · Engine (Turbine/Turboprop)
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